View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69097U 26135.89550219 +.00000000 +00000-0 +33805-4 0 00003
2 69097 97.5094 218.5703 0012926 275.6985 84.2771 15.10801700 07
| Epoch (UTC): | 15 May 2026 21:29:31 |
| Eccentricity: | 0.0012926 |
| inclination: | 97.5094° |
| perigee height: | 525 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 218.5703° |
| argument of perigee: | 275.6985° |
| revolutions per day: | 15.10801700 |
| mean anomaly at epoch: | 84.2771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|